View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60188U 26145.37694014 +.00000000 +00000-0 +13498-4 0 00007
2 60188 53.1586 143.5814 0001059 113.3104 246.8026 15.69709697 04
| Epoch (UTC): | 25 May 2026 09:02:47 |
| Eccentricity: | 0.0001059 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 143.5814° |
| argument of perigee: | 113.3104° |
| revolutions per day: | 15.69709697 |
| mean anomaly at epoch: | 246.8026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|